RU2686248C2 - Передняя часть авиационного двухконтурного газотурбинного двигателя и авиационный двухконтурный газотурбинный двигатель - Google Patents

Передняя часть авиационного двухконтурного газотурбинного двигателя и авиационный двухконтурный газотурбинный двигатель Download PDF

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Publication number
RU2686248C2
RU2686248C2 RU2016146533A RU2016146533A RU2686248C2 RU 2686248 C2 RU2686248 C2 RU 2686248C2 RU 2016146533 A RU2016146533 A RU 2016146533A RU 2016146533 A RU2016146533 A RU 2016146533A RU 2686248 C2 RU2686248 C2 RU 2686248C2
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RU
Russia
Prior art keywords
gas turbine
turbine engine
box
fan
front part
Prior art date
Application number
RU2016146533A
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English (en)
Russian (ru)
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RU2016146533A (ru
RU2016146533A3 (pt
Inventor
Натали НОВАКОВСКИ
Тома Ален Кристиан ВЕНСАН
Original Assignee
Сафран Эркрафт Энджинз
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Publication of RU2016146533A publication Critical patent/RU2016146533A/ru
Publication of RU2016146533A3 publication Critical patent/RU2016146533A3/ru
Application granted granted Critical
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/70—Disassembly methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/50—Bearings
    • F05D2240/53—Hydrodynamic or hydrostatic bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/90—Mounting on supporting structures or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/98—Lubrication
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • General Details Of Gearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Retarders (AREA)
  • Gear Transmission (AREA)
  • Gears, Cams (AREA)
RU2016146533A 2014-04-29 2015-04-27 Передняя часть авиационного двухконтурного газотурбинного двигателя и авиационный двухконтурный газотурбинный двигатель RU2686248C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1453890 2014-04-29
FR1453890A FR3020410B1 (fr) 2014-04-29 2014-04-29 Turbomachine d'aeronef a prelevement de puissance mecanique ameliore
PCT/FR2015/051133 WO2015166179A1 (fr) 2014-04-29 2015-04-27 Turbomachine d'aeronef a prelevement de puissance mecanique ameliore

Publications (3)

Publication Number Publication Date
RU2016146533A RU2016146533A (ru) 2018-05-29
RU2016146533A3 RU2016146533A3 (pt) 2018-09-26
RU2686248C2 true RU2686248C2 (ru) 2019-04-24

Family

ID=51210595

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016146533A RU2686248C2 (ru) 2014-04-29 2015-04-27 Передняя часть авиационного двухконтурного газотурбинного двигателя и авиационный двухконтурный газотурбинный двигатель

Country Status (8)

Country Link
US (1) US10895200B2 (pt)
EP (1) EP3137741B1 (pt)
CN (1) CN106255813B (pt)
BR (1) BR112016024728B1 (pt)
CA (1) CA2946710C (pt)
FR (1) FR3020410B1 (pt)
RU (1) RU2686248C2 (pt)
WO (1) WO2015166179A1 (pt)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2793638C1 (ru) * 2022-06-24 2023-04-04 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Газотурбинный двигатель с коробкой приводных агрегатов

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FR3020409B1 (fr) * 2014-04-29 2020-10-23 Snecma Assemblage pour turbomachine d'aeronef, comprenant un boitier de prelevement de puissance mecanique a acces simplifie
FR3045759B1 (fr) * 2015-12-21 2018-01-19 Safran Transmission Systems Mecanisme de transmission comprenant un organe d'accouplement, turbomachine equipee d'un tel mecanisme et procede de fonctionnement dudit mecanisme
US10526913B2 (en) * 2016-04-04 2020-01-07 United Technologies Corporation Anti-windmilling system for a gas turbine engine
FR3062421B1 (fr) * 2017-01-30 2021-04-16 Safran Aircraft Engines Dispositif d'entrainement d'une pompe a carburant pour turbomachine
FR3082553B1 (fr) * 2018-06-18 2020-09-25 Safran Aircraft Engines Ensemble pour turbomachine d'aeronef comportant un systeme ameliore de lubrification d'un reducteur d'entrainement de soufflante en cas d'autorotation de la soufflante
US11028778B2 (en) * 2018-09-27 2021-06-08 Pratt & Whitney Canada Corp. Engine with start assist
FR3098240B1 (fr) * 2019-07-03 2021-07-16 Safran Aircraft Engines Agencement de turbomachines d’aeronautique comprenant une pompe de lubrification entrainee par deux engrenages d’angle droit
FR3104208B1 (fr) 2019-12-06 2022-07-29 Safran Aircraft Engines Module de lubrification d’un réducteur de soufflante de turbomachine en phase d’autorotation de la soufflante
FR3109963B1 (fr) 2020-05-06 2022-10-07 Safran Aircraft Engines Module de lubrification d’un reducteur de soufflante de turbomachine en phase d’autorotation de la soufflante
FR3109960B1 (fr) * 2020-05-07 2022-07-15 Safran Trans Systems Relais d’accessoires
US11530617B2 (en) 2020-10-26 2022-12-20 Antheon Research, Inc. Gas turbine propulsion system
US11002146B1 (en) 2020-10-26 2021-05-11 Antheon Research, Inc. Power generation system
FR3136807A1 (fr) 2022-06-17 2023-12-22 Safran Transmission Systems Module de lubrification d’un poste de lubrification d’une turbomachine

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US4118997A (en) * 1976-08-14 1978-10-10 Rolls-Royce Limited Bevel gearing
US5845483A (en) * 1996-04-10 1998-12-08 General Electric Company Windmill engine starting system with fluid driven motor and pump
RU2157905C2 (ru) * 1994-01-17 2000-10-20 Акционерное общество закрытого типа "Энерготех" Газотурбинный двигатель
US20060248900A1 (en) * 2005-05-05 2006-11-09 Gabriel Suciu Accessory gearbox
US20110030385A1 (en) * 2009-08-07 2011-02-10 Rolls-Royce Plc propulsion unit

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FR2940247B1 (fr) * 2008-12-19 2011-01-21 Snecma Systeme d'helices contrarotatives entrainees par un train epicycloidal offrant une repartition de couple equilibree entre les deux helices
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US4118997A (en) * 1976-08-14 1978-10-10 Rolls-Royce Limited Bevel gearing
RU2157905C2 (ru) * 1994-01-17 2000-10-20 Акционерное общество закрытого типа "Энерготех" Газотурбинный двигатель
US5845483A (en) * 1996-04-10 1998-12-08 General Electric Company Windmill engine starting system with fluid driven motor and pump
US20060248900A1 (en) * 2005-05-05 2006-11-09 Gabriel Suciu Accessory gearbox
US20110030385A1 (en) * 2009-08-07 2011-02-10 Rolls-Royce Plc propulsion unit

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RU2793926C2 (ru) * 2019-02-21 2023-04-10 Сафран Эркрафт Энджинз Трансмиссионный вал, содержащий разрывную секцию, и способ защиты такого трансмиссионного вала от превышения крутящего момента
RU2793638C1 (ru) * 2022-06-24 2023-04-04 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Газотурбинный двигатель с коробкой приводных агрегатов

Also Published As

Publication number Publication date
RU2016146533A (ru) 2018-05-29
FR3020410B1 (fr) 2021-09-17
BR112016024728B1 (pt) 2022-09-06
RU2016146533A3 (pt) 2018-09-26
CN106255813A (zh) 2016-12-21
US20170051672A1 (en) 2017-02-23
EP3137741B1 (fr) 2020-09-09
CA2946710A1 (fr) 2015-11-05
FR3020410A1 (fr) 2015-10-30
CA2946710C (fr) 2022-07-26
BR112016024728A2 (pt) 2017-12-12
WO2015166179A1 (fr) 2015-11-05
US10895200B2 (en) 2021-01-19
EP3137741A1 (fr) 2017-03-08
CN106255813B (zh) 2019-05-07

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